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Determination of processing and test facility requirements for large solid rocket motors. Volume 2 - Task 2 - facility optimization Final reportCost optimization for 260-inch diameter solid rocket engine test facility
Document ID
19700027476
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lambert, W. L. (Aerojet Solid Propulsion Co. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72751
Report Number: NASA-CR-72751
Accession Number
70N36792
Funding Number(s)
CONTRACT_GRANT: NAS3-12041
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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